Author: M. J. Abbett
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 126
Book Description
The solution for the steady three-dimensional inviscid flow about supersonic blunt cones at angle of attack is obtained by coupling a direct time-dependent solution for the subsonic portion of the shock layer with steady state numerical afterbody solution. An outline is given covering the coupling scheme and the use of the resulting Fortran computer code.
Three-dimensional Inviscid Flow about Supersonic Blunt Cones at Angle of Attack
Author: M. J. Abbett
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 126
Book Description
The solution for the steady three-dimensional inviscid flow about supersonic blunt cones at angle of attack is obtained by coupling a direct time-dependent solution for the subsonic portion of the shock layer with steady state numerical afterbody solution. An outline is given covering the coupling scheme and the use of the resulting Fortran computer code.
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 126
Book Description
The solution for the steady three-dimensional inviscid flow about supersonic blunt cones at angle of attack is obtained by coupling a direct time-dependent solution for the subsonic portion of the shock layer with steady state numerical afterbody solution. An outline is given covering the coupling scheme and the use of the resulting Fortran computer code.
Three-dimensional Inviscid Flow about Supersonic Blunt Cones at Angle of Attack
Author: G. Moretti
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 88
Book Description
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 88
Book Description
Three-dimensional Inviscid Flow about Supersonic Blunt Cones at Angle of Attack
Author: G. Moretti
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 36
Book Description
Comparisons are made between the cylindrical and polar coordinate system used in determining the three-dimensional shock layer flow over the nose region of a blunted supersonic vehicle. Jusfification for the development of a polar coordinate system is given and an outline for such development is presented. Results from the polar coordinate system are given as is the limiting useful range.
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 36
Book Description
Comparisons are made between the cylindrical and polar coordinate system used in determining the three-dimensional shock layer flow over the nose region of a blunted supersonic vehicle. Jusfification for the development of a polar coordinate system is given and an outline for such development is presented. Results from the polar coordinate system are given as is the limiting useful range.
Three-dimensional Inviscid Flow about Supersonic Blunt Cones at Angle of Attack
Author: General Applied Science Laboratories (Westbury, Nassau County, N.Y.)
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 130
Book Description
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 130
Book Description
Three-dimensional Inviscid Flow about Supersonic Blunt Cones at Angle of Attack
Computational Fluid Mechanics and Heat Transfer
Author: Dale Anderson
Publisher: Taylor & Francis
ISBN: 1466578300
Category : Science
Languages : en
Pages : 763
Book Description
Thoroughly updated to include the latest developments in the field, this classic text on finite-difference and finite-volume computational methods maintains the fundamental concepts covered in the first edition. As an introductory text for advanced undergraduates and first-year graduate students, Computational Fluid Mechanics and Heat Transfer, Thi
Publisher: Taylor & Francis
ISBN: 1466578300
Category : Science
Languages : en
Pages : 763
Book Description
Thoroughly updated to include the latest developments in the field, this classic text on finite-difference and finite-volume computational methods maintains the fundamental concepts covered in the first edition. As an introductory text for advanced undergraduates and first-year graduate students, Computational Fluid Mechanics and Heat Transfer, Thi
Scientific and Technical Aerospace Reports
NASA Technical Paper
NASA Technical Paper
Author: United States. National Aeronautics and Space Administration
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 656
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 656
Book Description
Computational Fluid Mechanics and Heat Transfer, Second Edition
Author: Richard H. Pletcher
Publisher: CRC Press
ISBN: 9781560320463
Category : Science
Languages : en
Pages : 828
Book Description
This comprehensive text provides basic fundamentals of computational theory and computational methods. The book is divided into two parts. The first part covers material fundamental to the understanding and application of finite-difference methods. The second part illustrates the use of such methods in solving different types of complex problems encountered in fluid mechanics and heat transfer. The book is replete with worked examples and problems provided at the end of each chapter.
Publisher: CRC Press
ISBN: 9781560320463
Category : Science
Languages : en
Pages : 828
Book Description
This comprehensive text provides basic fundamentals of computational theory and computational methods. The book is divided into two parts. The first part covers material fundamental to the understanding and application of finite-difference methods. The second part illustrates the use of such methods in solving different types of complex problems encountered in fluid mechanics and heat transfer. The book is replete with worked examples and problems provided at the end of each chapter.